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Structural design optimization with survivability dependent constraints application: Primary wing box of a multi-role fighterThe superior survivability of a multirole fighter is dependent upon balanced integration of technologies for reduced vulnerability and susceptability. The objective is to develop a methodology for structural design optimization with survivability dependent constraints. The design criteria for optimization will be survivability in a tactical laser environment. The following analyses are studied to establish a dependent design relationship between structural weight and survivability: (1) develop a physically linked global design model of survivability variables; and (2) apply conventional constraints to quantify survivability dependent design. It was not possible to develop an exact approach which would include all aspects of survivability dependent design, therefore guidelines are offered for solving similar problems.
Document ID
19950022019
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dolvin, Douglas J.
(Wright Lab. Wright-Patterson AFB, OH, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Publication Information
Publication: FAA, Ninth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Volume 1
Subject Category
Aircraft Design, Testing And Performance
Accession Number
95N28440
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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